CN203550038U - Air-conditioner - Google Patents
Air-conditioner Download PDFInfo
- Publication number
- CN203550038U CN203550038U CN201320598392.7U CN201320598392U CN203550038U CN 203550038 U CN203550038 U CN 203550038U CN 201320598392 U CN201320598392 U CN 201320598392U CN 203550038 U CN203550038 U CN 203550038U
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- China
- Prior art keywords
- air
- assembly
- conditioner
- department
- chassis
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- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Abstract
The utility model is suitable for the field of air-conditioner and provides an air-conditioner. The air-conditioner comprises a chassis and an air-conditioner body arranged on the chassis, wherein the air-conditioner body comprises a rear shell, a panel and a top cover; the width of the chassis is less than or equal to the width of the air-conditioner body; an assembling part for mounting the rear shell is arranged along the periphery of the chassis; the two sides of the assembling part are protruded from the main body of the chassis; and decorative plates cover the two sides of the assembling part. In the air-conditioner provided by the utility model, the decorative plates are arranged on the chassis and are used for covering the two sides of the assembling part of the chassis, so that the fixing component for connecting the air-conditioner body with the chassis and the unclean structure of the assembling part are hidden and the appearance of the air-conditioner is clean and beautiful.
Description
Technical field
The utility model relates to air-conditioning technical field, relates in particular to a kind of air-conditioner.
Background technology
Chassis and the fuselage of existing split-floor type air conditioner are fixed by screw conventionally, and from lock-screw inside chassis, to avoid screw externally exposed, affect its outward appearance.But this kind of mode is only applicable to the type that chassis appearance and size is greater than or equal to fuselage size, when the appearance and size on chassis is less than fuselage size, cannot adopt fixed main body in this way, fixture easily exposes the outward appearance that affects air-conditioner.Therefore, be necessary to provide a kind of new fixed form, when chassis size is less than fuselage size, fixture and other the blowzy structure steganographies that fixed underpan and fuselage can be used, neat and artistic to guarantee air-conditioner outward appearance.
Utility model content
The purpose of this utility model is to provide a kind of chassis size to be less than or equal to the air-conditioner of fuselage size, and the fixture between its chassis and fuselage does not expose, and profile is neat and artistic.
The utility model is to realize like this, a kind of air-conditioner, comprise chassis and be arranged at the fuselage on described chassis, described fuselage comprises back cover, panel and top cover, the width on described chassis is less than or equal to the width of described fuselage, described chassis be provided with prolong that it around arranges in order to the department of assembly of described back cover to be installed, the both sides of described department of assembly protrude from the main part on described chassis, the both sides of described department of assembly respectively cover a decorative panel.
As optimal technical scheme of the present utility model:
Described decorative panel comprises the plate face of a bar shaped, and the two ends of described plate face are respectively provided with a hook, and described department of assembly is provided with the hanging hole coordinating with described hook.
The inner surface of described plate face is provided with at least one buckle, and described department of assembly is provided with and the described muscle position being clasped.
The inner surface of described plate face is provided with for limiting the locating piece of described decorative panel transverse shifting, and described department of assembly is provided with the positioning bar coordinating with described locating piece.
One side of the inner surface of described plate face is provided with for limiting the limited post of described decorative panel transverse shifting, and described department of assembly is provided with the spacing hole coordinating with described limited post.
Described department of assembly and the corresponding installing hole that is provided with on described back cover, described back cover and described department of assembly are passed described installing hole and are adopted nut check to fix in the outside of described department of assembly by bolt, and described nut is hidden by described decorative panel.
In described department of assembly, be also provided with a plurality of locating dowels, described back cover is provided with the locating hole passing for described locating dowel.
Described fuselage also comprises the wind component being arranged between described back cover and panel both sides.
The below of described wind component is also provided with lower panel.
Described decorative panel comprises the plate face of a bar shaped, and two ends and/or the inner surface of described plate face are provided with magnetic patch, and described department of assembly is irony department of assembly.
The air-conditioner that the utility model provides arranges decorative panel the both sides of the department of assembly on chassis is hidden in both sides, chassis, and then by connecting fuselage and the fixture on chassis and the untidy structure steganography of department of assembly, makes the profile of air-conditioner neat and artistic.
Accompanying drawing explanation
Fig. 1 is the surface structure schematic diagram of the air-conditioner that provides of the utility model embodiment;
Fig. 2 is the decomposition texture schematic diagram of the air-conditioner that provides of the utility model embodiment;
Fig. 3 is the enlarged drawing of a-quadrant in Fig. 2;
Fig. 4 is the decorative board structure schematic diagram () that the utility model embodiment provides;
Fig. 5 is the decorative board structure schematic diagram (two) that the utility model embodiment provides;
Fig. 6 is the enlarged drawing in B region in Fig. 5;
Fig. 7 is the chassis of air-conditioner and the part-structure schematic diagram of fuselage that the utility model embodiment provides;
Fig. 8 is the enlarged drawing in D region in Fig. 7;
Fig. 9 is the enlarged drawing in C region in Fig. 7;
Figure 10 is the plan structure schematic diagram on the chassis of the air-conditioner that provides of the utility model embodiment.
Figure 11 is the enlarged drawing in E region in Figure 10.
The specific embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearer, below in conjunction with drawings and Examples, the utility model is further elaborated.Should be appreciated that specific embodiment described herein is only in order to explain the utility model, and be not used in restriction the utility model.
Fig. 1 shows the surface structure schematic diagram of the air-conditioner that the utility model embodiment provides, and Fig. 2 shows the exploded view of the air-conditioner that the utility model embodiment provides, and for convenience of explanation, only shows the part relevant to the present embodiment.
With reference to figure 1,2, the air-conditioner that the utility model embodiment provides comprises chassis 1 and fuselage 2, and fuselage 2 is seated on chassis 1, and by fixture, is connected between chassis 1.Fuselage 2 comprises back cover 21, panel 22, top cover 23 and wind component 24 etc.In the present embodiment, shown in accompanying drawing 1,2, air-conditioner is the air-conditioner in a kind of pair of perfusion air channel, in the air-out of the left and right sides of air-conditioner, wind component 24 is arranged between back cover 21 and the both sides of panel 22, and be positioned at fuselage 2 first halves, below the wind component 24 of every side, be provided with a lower panel 25, can make up the vacancy of wind component 24 belows.And the air-conditioner that the utility model provides is not limited to the structure shown in Fig. 1,2, can also be other as air-conditioner of fuselage 2 front side air-outs etc.Please continue to refer to Fig. 2, chassis 1 comprise be located at its around for the fitting machine department of assembly 11 of shell 21 after one's death, the width of the main part on chassis 1 is less than the width of fuselage 2, the both sides of this department of assembly 11 protrude from the main part 12 on chassis 1, and the width between both sides equates with the width of fuselage 2 or be close.Between the back cover 21Yu department of assembly 11 of fuselage 2, by fixtures such as bolt, nuts, be connected, a part for fixture 3 is exposed to the outside on chassis 1.With reference to figure 7,9, when adopting bolt 31 and nut 32 fixedly during back cover 21, nut 32 is hidden by back cover 21, the nut of bolt 31 is exposed to outside, chassis, the nut that exposes to 11 both sides, department of assembly is easily in sight, and other blowzy structures of 11 both sides, department of assembly are also easily in sight, affect attractive in appearance.The both sides of the present embodiment department of assembly 11 of 1 on chassis respectively arrange a decorative panel 4, nut 32 fixtures such as grade and other blowzy structures are hidden, as Fig. 1,2,8.
On chassis, 1 both sides arrange decorative panel 4 by the both sides covering of the department of assembly on chassis 1 11 to the utility model embodiment, and then by connecting fuselage 2 and the fixture on chassis 1 and the untidy structure steganography of department of assembly 11, make the profile of air-conditioner neat and artistic.
With further reference to Fig. 4,5, this decorative panel 4 comprises the plate face 41 of a bar shaped, is respectively equipped with a hook 42 at the two ends of this plate face 41, simultaneously with reference to figure 8, is provided with the hanging hole 111 coordinating with this hook 42 in the department of assembly 11 on chassis 1.Further, on the inner surface of this panel 41, be also provided with at least one buckle 43, corresponding, in the department of assembly 11 on chassis 1, be provided with the muscle position 112 of matching with this buckle 43, as Fig. 3.When decorative panel 4 is installed, the hook 42 at decorative panel 4 two ends is hung in the One On The Chassis hanging hole 111, the buckle of decorative panel 4 43 is stuck on the muscle position 112 of department of assembly 11 simultaneously, to limit the free degree of decorative panel 4, realize being fixedly connected with of decorative panel 4 and chassis 1.Concrete, in hook 42 hanging holes 111 shown in Fig. 8, can limit decorative panel 4 and move downwards or outwards, buckle 43 is stuck in and on muscle position 112, can limits decorative panel 4 and move down.
With further reference to Fig. 5,6, one side of the inner surface of this decorative panel 4 is also provided with limited post 44, in chassis, 1 department of assembly 11 is provided with the spacing hole 113 coordinating with this limited post 44, as Figure 11, and the bottom-up transverse shifting that further limits decorative panel 4 in spacing hole 113 that penetrates of limited post 44.
With further reference to Fig. 5,6, the middle part of the inner surface of this decorative panel 4 is also provided with locating piece 45, corresponding, is also provided with the positioning bar 114 coordinating with this locating piece 45, as Fig. 3 in the department of assembly 11 on chassis 1.Concrete, locating piece 45 has can limit the retaining wall 451 that decorative panel 4 outwards moves relative to chassis, and positioning bar 114 is similar with the structure of above-mentioned muscle position 112, after locating piece 45 coordinates with positioning bar 114, positioning bar 114 is kept out in the inner side of retaining wall 451, prevents that decorative panel 4 from outwards moving.
With further reference to Fig. 9,10, in the department of assembly 11 on this chassis 1, can be provided with some locating dowels 115, locating dowel 115 is through in the locating hole 211 of fuselage back cover 21, in order to limit the transverse shifting of fuselage back cover 21.Simultaneously, department of assembly 11 is provided with installing hole 116 with the back cover 21 of fuselage simultaneously, and bolt 31 is bottom-up through installing hole 116, and the top of Bing department of assembly 11 adopts nut 32 and bolt 31 lockings, realize the fixing of fuselage 2 and chassis 1, and the lucky decorated plate 4 of the nut that expose 1 both sides, chassis hides.
In the present embodiment, locating dowel 115, installing hole 116 can prolong department of assembly 11 and be uniformly distributed, and as Figure 10, also can concentrate the both sides that are distributed in department of assembly 11, and the present embodiment is preferably uniformly distributed in department of assembly 11, so that the fixed effect of fuselage 2 is better.
As another kind of embodiment of the present utility model, one of the hook 41 of decorative panel 4, buckle 42, locating piece 44 or two or three can also be substituted by magnetic patch wherein, accordingly, on chassis, 1 11Shang relevant position, department of assembly arranges irony member or directly adopts irony department of assembly or irony chassis.And consider the possibility that magnetic patch magnetic weakens, the present embodiment preferably adopts the members such as above-mentioned hook, buckle to fix, or the mode being combined with above-mentioned partial component by part magnetic patch is fixedly connected with fuselage and chassis.
The foregoing is only preferred embodiment of the present utility model; not in order to limit the utility model; all any modifications of doing within spirit of the present utility model and principle, be equal to and replace and improvement etc., within all should being included in protection domain of the present utility model.
Claims (10)
1. an air-conditioner, it is characterized in that, comprise chassis and be arranged at the fuselage on described chassis, described fuselage comprises back cover, panel and top cover, the width on described chassis is less than or equal to the width of described fuselage, described chassis be provided with prolong that it around arranges in order to the department of assembly of described back cover to be installed, the both sides of described department of assembly protrude from the main part on described chassis, the both sides of described department of assembly respectively cover a decorative panel.
2. air-conditioner as claimed in claim 1, is characterized in that, described decorative panel comprises the plate face of a bar shaped, and the two ends of described plate face are respectively provided with a hook, and described department of assembly is provided with the hanging hole coordinating with described hook.
3. air-conditioner as claimed in claim 2, is characterized in that, the inner surface of described plate face is provided with at least one buckle, and described department of assembly is provided with and the described muscle position being clasped.
4. air-conditioner as claimed in claim 2, is characterized in that, the inner surface of described plate face is provided with for limiting the locating piece of described decorative panel transverse shifting, and described department of assembly is provided with the positioning bar coordinating with described locating piece.
5. air-conditioner as claimed in claim 2, is characterized in that, a side of the inner surface of described plate face is provided with for limiting the limited post of described decorative panel transverse shifting, and described department of assembly is provided with the spacing hole coordinating with described limited post.
6. the air-conditioner as described in claim 1 to 5 any one, it is characterized in that, described department of assembly and the corresponding installing hole that is provided with on described back cover, described back cover and described department of assembly are passed described installing hole and are adopted nut check to fix in the outside of described department of assembly by bolt, and described nut is hidden by described decorative panel.
7. air-conditioner as claimed in claim 6, is characterized in that, is also provided with a plurality of locating dowels in described department of assembly, and described back cover is provided with the locating hole passing for described locating dowel.
8. the air-conditioner as described in claim 1 to 5,7 any one, is characterized in that, described fuselage also comprises the wind component being arranged between described back cover and panel both sides.
9. air-conditioner as claimed in claim 8, is characterized in that, the below of described wind component is also provided with lower panel.
10. air-conditioner as claimed in claim 1, is characterized in that, described decorative panel comprises the plate face of a bar shaped, and two ends and/or the inner surface of described plate face are provided with magnetic patch, and described department of assembly is irony department of assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320598392.7U CN203550038U (en) | 2013-09-26 | 2013-09-26 | Air-conditioner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320598392.7U CN203550038U (en) | 2013-09-26 | 2013-09-26 | Air-conditioner |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203550038U true CN203550038U (en) | 2014-04-16 |
Family
ID=50468148
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320598392.7U Expired - Lifetime CN203550038U (en) | 2013-09-26 | 2013-09-26 | Air-conditioner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203550038U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104764184A (en) * | 2015-03-31 | 2015-07-08 | 广东美的制冷设备有限公司 | Anti-thrust structure for air conditioner indoor unit and air conditioner indoor unit device |
-
2013
- 2013-09-26 CN CN201320598392.7U patent/CN203550038U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104764184A (en) * | 2015-03-31 | 2015-07-08 | 广东美的制冷设备有限公司 | Anti-thrust structure for air conditioner indoor unit and air conditioner indoor unit device |
| CN104764184B (en) * | 2015-03-31 | 2019-01-22 | 广东美的制冷设备有限公司 | Thrust structure and air conditioner room unit device for air conditioner room unit |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20140416 |
|
| CX01 | Expiry of patent term |